1.
Error Calibration of SINS Based on Rate Offset Frequency Ring Laser Gyro
速率偏频激光捷联惯导系统的误差标定
2.
Attitude Algorithm with Incremental Angle of RLG SINS
激光捷联惯导系统角增量输入姿态算法
3.
Active Disturbance Rejection Control of the Stabilizing Loop for Roll-Isolated Laser Gyro Strap-Down Inertial Navigation System
横滚隔离激光捷联惯导系统稳定回路自抗扰控制
4.
Research on Inertial Strapdown System with Mechanically Dithered Ring Laser Gyroscope;
机抖激光陀螺捷联惯导系统的初步探索
5.
Research on Vibration Error of Mechanically Dithered Ring Laser Gyro and Strapdown Inertial Navigation System;
机抖激光陀螺及捷联惯导系统振动误差研究
6.
Research on Error Compensation Technology of Mechanically Dithered Ring Laser Gyro SINS;
机抖激光陀螺捷联惯导系统误差补偿技术研究
7.
Design and Realization of LSINS Data Acquisition;
激光陀螺捷联惯导系统数据采集的设计与实现
8.
Power spectrum analysis for laser gyro damping system of strapdown inertial navigation
激光陀螺捷联惯导系统减振功率谱分析
9.
The Development of Miniaturization Navigation CPU Board Based on the Technology of DSP and CPLD Applied in Laser Gyro Strapdown Inertial Navigation Systems;
基于DSP和CPLD技术的激光陀螺捷联惯导系统小型化导航CPU板的研制
10.
Research on Integrated Navigation and Zero Velocity Update Technology of Strapdown Inertial Navigation System with Ring Laser Gyroscope
激光陀螺捷联惯性导航系统组合导航及零速修正技术研究
11.
The Research of Hardware of Strapdown Inertial Navigation System Based on FOG;
光纤陀螺捷联惯导系统硬件电路研究
12.
The Study on Temperature Effect Compensation for Fiber-optic Strapdown Inertial Navigation System
光纤捷联惯导系统温度效应补偿研究
13.
Research on Strapdown Inertial Navigation System with Mechanically Dithered Ring Laser Gyroscope and Its Real-time Temperature Compensating Approach;
二频机抖激光陀螺捷联惯导系统及其实时温度补偿方法的研究
14.
The Study of Algorithm and Simulation for Ring Laser Gyro Strapdown Inertial Navigation System for Rocket;
箭载激光陀螺捷联惯导系统算法研究与仿真设计
15.
Signal Detecting and Processing of Strapdown Inertial Navigation System with Ring Laser Gyroscope Based on FPGA
基于FPGA的激光陀螺捷联惯导系统信号的检测与处理
16.
Calibration and optimal compensation for size effect parameters of laser gyro SINS
激光陀螺捷联惯导系统尺寸效应参数标定与优化补偿
17.
strap-down inertial navigation system
捷联式惯性导航系统
18.
Research on Error Excitatedation in Flexible SINS Caused by Airborne Installation Way;
挠性捷联惯导系统机载安装方式误差激励研究